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Pressure Disturbances

Of course, the best remedy to minimize downstream instabilities is to minimize the input disturbance. Pressure initiation is thus incorporated, and the simplest and most effective way of achieving this is by vertical screw... [Pg.721]

In weakly consolidated, stratified sediments, the injection pressure must be controlled so that the surrounding formation is not fractured. If fracturing occurs, there is usually a severe loss in hydraulic conductivity because the bedding planes are disturbed. Pressures that will cause fracturing range from a low of 0.5 psi/ft of depth for poorly consolidated coastal plain sediments, to 1.2 psi/ft depth for crystalline rock. For most recharge wells in unconsolidated sediments, the injection pressure should be carefully controlled so that the positive head (in psi at the surface) does not exceed 0.2 x h, where h is the depth (in ft) from the ground surface to the top of the screen or filter pack. [Pg.260]

This method is particularly simple to apply in the case of a point force f. The (disturbance) pressure must be a decaying harmonic ftmction that is linear in f and a true scalar. Hence,... [Pg.546]

In the example of the dehydrogenation reaction above, the mass flows are assumed invariant, their composition is not disturbed. Pressure and temperature are dictated by the thermodynamics of the system to attain a certain conversion of the feed. An alternative form of PI (process intensification) can be seen when one selectively removes one of the reaction products to shift the equilibrium and intensify the process. The combination of reaction and separation is a key example of PI. The literature aboimds with schemes to accomplish this. Its commercial use, however, is limited to a small number of cases. Following are examples, successful and not so successful, of this mode of operation ... [Pg.50]

The second step is the linearization of the governing flow equations and boundary conditions assuming the flow to be only slightly disturbed. The momentum equation so linearized is given by Eq. (10.4.3), with the excess or disturbance pressure and u the disturbance velocity. The continuity equation for the disturbance velocity is as before, V (/> = 0. The natural coordinates for the problem are the cylindrical coordinates (r, 6, z) in which Laplace s equation takes the form... [Pg.315]

Thus, for this extreme event, we observe the full combination of hazardous conditions (factors) responsible for the formation catastrophic oscillations inside Nagasaki Bay (1) A pronounced atmospheric disturbance (pressure jump of 2-6 hPa), (2) propagating toward the bay with (3) near-resonant phase speed of 31m/s this disturbance resonantly generated open-sea long waves with selected (over the shelf) 36 min period that matched (4) the fundamental 35-min period of the bay that has (5) high Q-factor and well-defined resonant properties. As a result, 3 cm ocean waves in the source area resulted in 478 cm waves at the head of the bay (Fig. 9.4). [Pg.231]

Numerical solutions depend strongly on the choice of grid. Using any reservoir simulator, compute the flowfields about stand-alone fractures and shales, say, centered in a large computational box. Do your results satisfy the symmetries and antisymmetries derived here for pressure and normal velocity A single straight shale in an infinite medium has a perfectly antisymmetric disturbance pressure field. Show that this antisymmetry is... [Pg.50]

The commercial form of Cartesian manostat, model 7A, is depicted in Fig. II, 23, 7 it is normally charged with mercury except for very low pressures when di-w-butyl phthalate is employed. The manostat is highly sensitive in its action furthermore, once the pressure has been set in the instrument, the system may be shut down without disturbing the setting. [Pg.116]

Schemes to control the outlet temperature of a process furnace by adjusting the fuel gas flow are shown in Figure 13. In the scheme without cascade control (Fig. 13a), if a disturbance has occurred in the fuel gas supply pressure, a disturbance occurs in the fuel gas flow rate, hence, in the energy transferred to the process fluid and eventually to the process fluid furnace outlet temperature. At that point, the outlet temperature controller senses the deviation from setpoint and adjusts the valve in the fuel gas line. In the meantime, other disturbances may have occurred in the fuel gas pressure, etc. In the cascade control strategy (Fig. 13b), when the fuel gas pressure is disturbed, it causes the fuel gas flow rate to be disturbed. The secondary controller, ie, the fuel gas flow controller, immediately senses the deviation and adjusts the valve in the fuel gas line to maintain the set fuel gas rate. If the fuel gas flow controller is well tuned, the furnace outlet temperature experiences only a small disturbance owing to a fuel gas supply pressure disturbance. Schemes to control the outlet temperature of a process furnace by adjusting the fuel gas flow are shown in Figure 13. In the scheme without cascade control (Fig. 13a), if a disturbance has occurred in the fuel gas supply pressure, a disturbance occurs in the fuel gas flow rate, hence, in the energy transferred to the process fluid and eventually to the process fluid furnace outlet temperature. At that point, the outlet temperature controller senses the deviation from setpoint and adjusts the valve in the fuel gas line. In the meantime, other disturbances may have occurred in the fuel gas pressure, etc. In the cascade control strategy (Fig. 13b), when the fuel gas pressure is disturbed, it causes the fuel gas flow rate to be disturbed. The secondary controller, ie, the fuel gas flow controller, immediately senses the deviation and adjusts the valve in the fuel gas line to maintain the set fuel gas rate. If the fuel gas flow controller is well tuned, the furnace outlet temperature experiences only a small disturbance owing to a fuel gas supply pressure disturbance.
J ct Spra.y, The mechanism that controls the breakup of a Hquid jet has been analy2ed by many researchers (22,23). These studies indicate that Hquid jet atomisation can be attributed to various effects such as Hquid—gas aerodynamic interaction, gas- and Hquid-phase turbulence, capillary pinching, gas pressure fluctuation, and disturbances initiated inside the atomiser. In spite of different theories and experimental observations, there is agreement that capillary pinching is the dominant mechanism for low velocity jets. As jet velocity increases, there is some uncertainty as to which effect is most important in causing breakup. [Pg.330]

Vacuum and Atmosphere Melting. A coreless high frequency induction furnace is enclosed in a container or tank which can be either evacuated or filled with a gaseous atmosphere of any desired composition or pressure. Provision is made for additions to the melt, and tilting the furnace to pour its contents into an ingot mold also enclosed in the tank or container without disturbing the vacuum or atmosphere in the tank (Fig. 2). [Pg.375]

Better antihypertensive effect of P-adrenoceptor blockers is found in patients having high PRA and most are not efficacious in patients having low PRA or in elderly patients. P-Adrenoceptor blockers usually lower arterial blood pressure about 10 mm Hg (1.3 kPa). Side effects include lethargy, dyspnea, nausea, dizziness, headache, impotency, cold hands and feet, vivid dreams and nightmares, bronchospasm, bradycardia, and sleep disturbances. [Pg.141]

Verapamil (Table 1), the first slow channel calcium blocker synthesized to selectively inhibit the transmembrane influx of calcium ions into cells, lowers blood pressure in hypertensive patients having good organ perfusion particularly with increased renal blood flow. Sustained-release verapamil for once a day dosing is available for the treatment of hypertension. Constipation is a prominent side effect. Headache, dizziness, and edema are frequent and verapamil can sometimes cause AV conduction disturbances and AV block. Verapamil should not be used in combination with -adrenoceptor blockers because of the synergistic negative effects on heart rate and contractile force. [Pg.142]

V/c is the ratio of fluid velocity to the speed of sound or aeoustie veloeity, c. The speed of sound is the propagation velocity of infinitesimal pressure disturbances and is derived from a momentum balance. The compression caused by the pressure wave is adiabatic and frictionless, and therefore isentropic. [Pg.648]

Disturbance or load variable Sound pressure level Manipulated variable Number of constraints Mass flow Mass of reactants Molecular weight... [Pg.717]

A regulator is a compact device that maintains the process variable at a specific value in spite of disturbances in load flow. It combines the functions of the measurement sensor, controher, and final control element into one self-contained device. Regulators are available to control pressure, differential pressure, temperature, flow, hquid level, and other basic process variables. They are used to control the differential across a filter press, heat exchanger, or orifice plate. Regulators are used for monitoring pressure variables for redundancy, flow check, and liquid surge relief. [Pg.793]

Disturbances upstream of the probe can cause large errors, in part because of the turbulence generated and its effect on the static-pressure measurement. A calming section of at least 50 pipe diameters is desirable. If this is not possible, the use of straightening vanes or a honeycomb is advisable. [Pg.887]

In most solids, the sound speed is an increasing function of pressure, and it is that property that causes a compression wave to steepen into a shock. The situation is similar to a shallow water wave, whose velocity increases with depth. As the wave approaches shore, a small wavelet on the trailing, deeper part of the wave moves faster, and eventually overtakes similar disturbances on the front part of the wave. Eventually, the water wave becomes gravitationally unstable and overturns. [Pg.18]

For a shock wave in a solid, the analogous picture is shown schematically in Fig. 2.6(a). Consider a compression wave on which there are two small compressional disturbances, one ahead of the other. The first wavelet moves with respect to its surroundings at the local sound speed of Aj, which depends on the pressure at that point. Since the medium through which it is propagating is moving with respect to stationary coordinates at a particle velocity Uj, the actual speed of the disturbance in the laboratory reference frame is Aj - -Ui- Similarly, the second disturbance advances at fl2 + 2- Thus the second wavelet overtakes the first, since both sound speed and particle velocity increase with pressure. Just as a shallow water wave steepens, so does the shock. Unlike the surf, a shock wave is not subject to gravitational instabilities, so there is no way for it to overturn. [Pg.18]

In materials that support shock waves, the sound speed increases with pressure. It is this same property that causes rarefactions to spread out as they progress. In Fig 2.6(b), an unloading wave is shown propagating into a stationary material with some initial pressure Pq. This time, we consider the evolution of two small decompressional disturbances. The first disturbance moves at the local sound speed of a, into its surroundings, which have begun... [Pg.21]


See other pages where Pressure Disturbances is mentioned: [Pg.136]    [Pg.526]    [Pg.129]    [Pg.175]    [Pg.334]    [Pg.140]    [Pg.136]    [Pg.526]    [Pg.129]    [Pg.175]    [Pg.334]    [Pg.140]    [Pg.126]    [Pg.804]    [Pg.141]    [Pg.249]    [Pg.91]    [Pg.98]    [Pg.100]    [Pg.269]    [Pg.193]    [Pg.95]    [Pg.251]    [Pg.70]    [Pg.72]    [Pg.308]    [Pg.330]    [Pg.88]    [Pg.146]    [Pg.658]    [Pg.762]    [Pg.884]    [Pg.884]    [Pg.1470]    [Pg.2328]    [Pg.2499]    [Pg.20]   
See also in sourсe #XX -- [ Pg.334 ]




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